The present invention relates to a method for real-time prediction of an intercept point of a guided missile capable of predicting an impact point of a missile in real time, comprising the steps of: deriving a distance of flight considering a flight path of a missile in inputting a flight condition; The step of linearizing the flight speed of the missile and integrating it during the remaining flight time to analytically derive the flight distance considering the flight speed of the missile; Deriving an intercept point relationship based on the derived distance in consideration of the trajectory of the guided missile and the flight distance in consideration of the speed of the missile; Calculating a solution of the derived intercept point relationship; And estimating in real time an intercept prediction point and a remaining flight time using the calculated intercept point correlation.
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